首页 | 本学科首页   官方微博 | 高级检索  
文章检索
  按 检索   检索词:      
出版年份:   被引次数:   他引次数: 提示:输入*表示无穷大
  收费全文   138篇
  免费   26篇
  国内免费   49篇
航空   62篇
航天技术   77篇
综合类   13篇
航天   61篇
  2024年   3篇
  2022年   3篇
  2021年   2篇
  2020年   8篇
  2019年   7篇
  2018年   10篇
  2017年   6篇
  2016年   4篇
  2015年   6篇
  2014年   15篇
  2013年   4篇
  2012年   14篇
  2011年   17篇
  2010年   13篇
  2009年   16篇
  2008年   9篇
  2007年   9篇
  2006年   7篇
  2005年   7篇
  2004年   5篇
  2003年   5篇
  2002年   4篇
  2001年   5篇
  2000年   4篇
  1999年   2篇
  1998年   3篇
  1997年   3篇
  1996年   5篇
  1995年   1篇
  1994年   2篇
  1993年   4篇
  1992年   3篇
  1991年   3篇
  1990年   2篇
  1989年   1篇
  1988年   1篇
排序方式: 共有213条查询结果,搜索用时 109 毫秒
81.
Solar particle events leading to important increase of particle fluxes at energies of order of magnitude ranging from MeV to GeV constitute an important hazard for space missions. They may lead to effects seen in microelectronics or damage to solar cells and constitute a potential hazard for manned missions. Cumulative damage is commonly expressed as a function of fluence which is defined as the integral of the flux over time. A priori deterministic estimates of the expected fluence cannot be made because over the time scale of a space mission, the fluence can be dominated by the contribution of a few rare and unpredictable high intensity events. Therefore, statistical approaches are required in order to estimate fluences likely to be encountered by a space mission in advance. This paper extends work done by Rosenqvist et al. [Rosenqvist, L., Hilgers, A., Evans, H., Daly, E., Hapgood, M., Stamper, R., Zwickl, R., Bourdarie, S., Boscher, D. Toolkit for updating interplanetary proton-cumulated fluence models. J. Spacecraft Rockets, 42(6), 1077–1090, 2005] to describe an updated predictive engineering model for the proton interplanetary fluence with energies >30 MeV. This model is derived from a complete list of solar proton fluences based on data from a number of calibrated sources covering almost three solar cycles.  相似文献   
82.
From 1 January 1986 through 1 January 2008, GOES satellites recorded 170 solar proton events. For 169 of these events, we estimated effective and equivalent dose rates and doses of galactic cosmic radiation (GCR) and solar cosmic radiation (SCR), received by aircraft occupants on simulated high-latitude flights. Dose rate and dose estimates that follow are for altitudes 30, 40, 50, and 60 kft, in that order.  相似文献   
83.
Hourly magnetic readings of H and D from six geomagnetic observatories in Finland and Russia were utilized for analysis of the time behavior of the extreme space weather event of August/September 1859. The observatories cover about 200° in longitude and magnetic latitudes 45–60°N.  相似文献   
84.
FY—1C卫星空间粒子成分监测器及其探测结果   总被引:1,自引:0,他引:1  
简要介绍了FY-1C星空间粒子成分监测器的任务目标、工作原理、创新特色及在轨探测结果。空间粒子成分监测器用于卫星轨道空间的带电粒子辐射监测,为卫星的在轨安全和抗辐射加固设计服务。监测器在世界上实现用1套传感器完成对高能电子、质子、α粒子至铁离子的全成分监测,使我国首次获得了870km高太阳同步轨道全空间的各种重离子分布、质子能谱分布和电子通量分布,捕捉到大量的地磁暴和太阳质子事件,获得了批重要的探测成果。  相似文献   
85.
SMP2仿真引擎的多核并行化   总被引:1,自引:0,他引:1  
苏年乐  周鸿伟  李群  王维平 《宇航学报》2010,31(7):1883-1891
仿真模型可移植性规范2(SMP2)是由欧洲航天局制定并得到广泛应用的仿真模型开发与集  相似文献   
86.
本文以某型航电任务系统研发为背景,介绍了几种经典体系结构风格的设计特点和应用。理论和研发实践相结合,项目的顺利推进证明了软件体系结构风格的分析对明确设计思路和指导代码开发具有重要意义,加快了软件研发的进度,保证软件质量,同时又增加了系统的可扩展性,降低研发成本。  相似文献   
87.
Ionospheric scintillation variations are studied using GPS measurements at the low latitude station of Shenzhen (22.59°N, 113.97°E), situated under the northern crest of the equatorial anomaly region, from the Chinese Meridian Project. The results are presented for data collected during the current phase of rising solar activity (low to high solar activity) from December 2010 to April 2014. The results show that GPS scintillation events were largely a nighttime phenomenon during the whole observation period. Scintillation events mainly occurred along the inner edge of the northern crest of the equatorial anomaly in China. The occurrence of scintillations in different sectors of the sky was also investigated, and the results revealed that it is more likely for the scintillations to be observed in the west sector of the sky above Shenzhen. During the present period of study, a total number of 512 total electron content (TEC) depletions and 460 lock loss events were observed. In addition, both of these events are likely to increase during periods of high solar activity, especially because the strong scintillations are often simultaneously accompanied by TEC depletions and lock losses by GPS receivers.  相似文献   
88.
李勇华  高为炳 《航空学报》1992,13(11):647-653
 基于状态时间的概念,在Ramadge-Wonham模型的基础上提出了一种新的实时离散事件系统模型。在控制目标是保持某给定谓词在闭环系统状态轨迹上为真的情况下,给出了实时控制不变性的定义。研究表明,对这类系统,存在一个状态反馈控制器使给定谓词在闭环系统状态轨迹上保持为真的充要条件是该谓词是实时控制不变的。证明了给定谓词所含的最大实时控制不变子谓词的存在性并给出了计算方法。最后,给出一个例子来说明有关结果。  相似文献   
89.
Abstract

Events, like objects, can be decomposed into parts. Path, the spatiotemporal trajectory of an object during an event, is the most commonly labeled event feature across the world's languages, provides important social information, and is increasingly central to theories of general event segmentation. However, little is understood about how adults visually segment paths. We apply theories developed for object segmentation to help understand path segmentation. Overall subjects segmented equivalent object shapes and event paths in similar ways following patterns predicted by Singh and Hoffman's (2001) Singh, M. and Hoffman, D. D. 2001. “Parts-based representations of visual shape and implications for visual cognition.”. In From fragments to objects—Segmentation and grouping in vision Edited by: Shipley, T. F. and Kellman, P. J. 401459. New York, NY: Elsevier Science..  [Google Scholar] geometric analysis of object parts. There were two notable differences between object and event segmentation: (1) event parsing occurred at points of negative curvature minima and positive curvature maxima as opposed to simply negative curvature minima; and (2) event parsing was more frequent and variable than object parsing. Implications of these results for event perception and categorization are discussed.  相似文献   
90.
卢万杰  徐青  蓝朝桢  吕亮 《宇航学报》2020,41(8):1105-1114
针对空间目标态势威胁响应和预警研究不完善的问题,为实现空间目标行为和事件的智能推理、实时响应和主动预警,保障航天活动和空间利益,提出面向行为与事件的空间目标态势本体模型(BEO-SO2)。基于基本形式本体(BFO),构建空间目标态势行为与事件本体模型。在统一时空框架下建立空间目标关系模型,实现空间目标行为执行和事件发生过程的动态推演。以空间目标碰撞威胁为背景,设计对象实体等级体系和碰撞威胁行为与事件要素,建立碰撞威胁推理规则,基于空间目标态势行为与事件本体进行实现、验证与展示。结果表明,空间目标态势行为与事件本体能够实现空间目标碰撞威胁的等级推理与预警,并指导进一步的空间活动,为航天任务与空间活动提供有效保障。  相似文献   
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号